Explore topic-wise MCQs in Rocket Propulsion.

This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Rocket Propulsion knowledge and support exam preparation. Choose a topic below to get started.

Explore topic-wise MCQs in Rocket Propulsion.

Determine the normal force coefficient of a rocket having a maximum frontal area of 0.2 m2, flying at sea level with a velocity of 100 m/s. Consider the center of gravity to be ahead of the center of pressure by 0.5 m and the corrective moment coefficient to be 2.5.

The point on the rocket where all the aerodynamic forces balance is called as the ______________

For an airplane undergoing a steady pull-up maneuver along a curved flight path of the constant angle of attack, constant pitch rate of 20°/s, and having a radius of curvature of 150 m, determine the flight velocity.

For some type of flying vehicle applications, a low-speed roll is given to avoid thrust vector deviations.

For a satellite revolving around the earth in a circular orbit at an altitude of 350 km, determine the orbital velocity.

Determine the period of revolution of an artificial satellite in a circular orbit of altitude 350 km.

Which of the following can be spin-stabilized?

Which of the following statements is true for the center of gravity (cog) and the center of pressure (cop) location along the axis of a fuel powered aircraft?

Suppose an aircraft trimmed at a 10° angle of attack faces a gust that changes the angle of attack to 15°. What is the nature of the moment required to bring it back to the trimmed condition?

Stability of a flying vehicle cannot be ensured by __________